A general method has been developed which permits the transfer of a spacecraft from a highly elliptic and generally oriented Earth orbit to a specified escape direction and energy.
Planetary Missions from GTO Using Earth and Moon Gravity Assists
AIAA Astrodynamics Specialist Conference
1998-08-10
Aufsatz (Konferenz)
Keine Angabe
Englisch
Trajectory Design in the Sun-Earth-Moon System Using Lunar Gravity Assists
Online Contents | 1998
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